EP0433582A1 - Préparation de structures en nid d'abeille à obturation sélective de canaux - Google Patents

Préparation de structures en nid d'abeille à obturation sélective de canaux Download PDF

Info

Publication number
EP0433582A1
EP0433582A1 EP90119094A EP90119094A EP0433582A1 EP 0433582 A1 EP0433582 A1 EP 0433582A1 EP 90119094 A EP90119094 A EP 90119094A EP 90119094 A EP90119094 A EP 90119094A EP 0433582 A1 EP0433582 A1 EP 0433582A1
Authority
EP
European Patent Office
Prior art keywords
channels
honeycomb
face
ceramic
green
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP90119094A
Other languages
German (de)
English (en)
Inventor
Leslie Eugene Hampton
David Fred Thompson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Corning Inc
Original Assignee
Corning Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Corning Inc filed Critical Corning Inc
Publication of EP0433582A1 publication Critical patent/EP0433582A1/fr
Withdrawn legal-status Critical Current

Links

Images

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/02—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust
    • F01N3/021—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust by means of filters
    • F01N3/022—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust by means of filters characterised by specially adapted filtering structure, e.g. honeycomb, mesh or fibrous
    • F01N3/0222—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust by means of filters characterised by specially adapted filtering structure, e.g. honeycomb, mesh or fibrous the structure being monolithic, e.g. honeycombs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D29/00—Filters with filtering elements stationary during filtration, e.g. pressure or suction filters, not covered by groups B01D24/00 - B01D27/00; Filtering elements therefor
    • B01D29/11—Filters with filtering elements stationary during filtration, e.g. pressure or suction filters, not covered by groups B01D24/00 - B01D27/00; Filtering elements therefor with bag, cage, hose, tube, sleeve or like filtering elements
    • B01D29/111—Making filtering elements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D29/00—Filters with filtering elements stationary during filtration, e.g. pressure or suction filters, not covered by groups B01D24/00 - B01D27/00; Filtering elements therefor
    • B01D29/11—Filters with filtering elements stationary during filtration, e.g. pressure or suction filters, not covered by groups B01D24/00 - B01D27/00; Filtering elements therefor with bag, cage, hose, tube, sleeve or like filtering elements
    • B01D29/31—Self-supporting filtering elements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D29/00—Filters with filtering elements stationary during filtration, e.g. pressure or suction filters, not covered by groups B01D24/00 - B01D27/00; Filtering elements therefor
    • B01D29/50—Filters with filtering elements stationary during filtration, e.g. pressure or suction filters, not covered by groups B01D24/00 - B01D27/00; Filtering elements therefor with multiple filtering elements, characterised by their mutual disposition
    • B01D29/52—Filters with filtering elements stationary during filtration, e.g. pressure or suction filters, not covered by groups B01D24/00 - B01D27/00; Filtering elements therefor with multiple filtering elements, characterised by their mutual disposition in parallel connection
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D46/00—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
    • B01D46/10—Particle separators, e.g. dust precipitators, using filter plates, sheets or pads having plane surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B28—WORKING CEMENT, CLAY, OR STONE
    • B28B—SHAPING CLAY OR OTHER CERAMIC COMPOSITIONS; SHAPING SLAG; SHAPING MIXTURES CONTAINING CEMENTITIOUS MATERIAL, e.g. PLASTER
    • B28B11/00—Apparatus or processes for treating or working the shaped or preshaped articles
    • B28B11/003—Apparatus or processes for treating or working the shaped or preshaped articles the shaping of preshaped articles, e.g. by bending
    • B28B11/006—Making hollow articles or partly closed articles
    • C—CHEMISTRY; METALLURGY
    • C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B38/00—Porous mortars, concrete, artificial stone or ceramic ware; Preparation thereof
    • C04B38/0006—Honeycomb structures
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01D—SEPARATION
    • B01D2201/00—Details relating to filtering apparatus
    • B01D2201/46—Several filtrate discharge conduits each connected to one filter element or group of filter elements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N2330/00—Structure of catalyst support or particle filter
    • F01N2330/06—Ceramic, e.g. monoliths
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/10—Methods of surface bonding and/or assembly therefor
    • Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
    • Y10T156/1056—Perforating lamina
    • Y10T156/1057—Subsequent to assembly of laminae

Definitions

  • This invention relates to the preparation of a ceramic honeycomb structure having channels that are selectively sealed at alternate faces of the honeycomb.
  • the honeycombs are useful in a variety of filtering, separating, or concentrating operations in which a work fluid or component thereof is intended to pass through the walls of the channels.
  • the otherwise open channel must be selectively and alternately sealed at one end or the other to prevent the gas from merely passing through the channel itself.
  • the preparation of a honeycomb with such alternately sealed channels cannot be accomplished in a single extrusion step and requires at least one further operation performed on a green or fired open-channelled honeycomb.
  • U.S. Patent 4,283,210 in which the selective sealing of channels is effected by bending and bonding the partition walls of given channels at one of the end faces of a green ceramic honeycomb body, and performing the same operation to the remaining channels at the other end face of the body.
  • Patent 4,329,162 also discloses ceramic honeycomb filters in which selective seals are provided to the inlet and outlet channels by injecting a sinterable material or other sealing cement into the appropriate ends of the channels to form a "checkerboard" array of open/closed channels at each end face.
  • the present invention provides a method for the preparation of a ceramic honeycomb body having selectively sealed channels for use in operations in which a fluid or component of the fluid is intended to be passed through the partition walls of a multi-channeled honeycomb.
  • the starting point for the preparation method is a green ceramic honeycomb body, as prepared by methods known in the art, which body has an inlet face and an outlet face and a plurality of substantially parallel channels extending through the honeycomb between the faces.
  • a moistened, substantially flat, green ceramic body is then fitted against each of said faces of the honeycomb to form a substantially integral end cap over the faces, resulting in the sealing of the channel openings therein.
  • the ceramic material of the end caps and that of the honeycomb body itself are chosen so as to have substantially similar thermal expansion properties, and more preferably are the same ceramic material.
  • the composite honeycombs are coated with an electrically conductive material to form one electrode connecting the inlet face and the channels open to that face and a second electrode connecting the outlet face and the channels open to it. Structures of this embodiment are useful in the process of oxygen concentration or as fuel cells.
  • Figure 1 is a perspective view of a ceramic composite honeycomb of the invention having selectively sealed channels.
  • Figure 2 is a partial cross-section of the honeycomb of Figure 1 along line A-A.
  • the present invention provides a practical and efficient method for the preparation of ceramic honeycombs having channels that are hermetically sealed at one face or the other of the honeycomb.
  • certain of the channels are inlet channels for a stream of work fluid and the remaining channels are outlet channels for the filtered work stream or components thereof that have passed through the channel partition walls.
  • the honeycombs are useful as filters, particulate traps (such as for diesel engines), or catalyst structures and supports, or as the solid electrolyte medium for fuel cells or gas concentrators or detectors, or in other operations in which a fluid work stream or components of the stream are intended to pass through the partition walls of a honeycomb.
  • a green ceramic honeycomb having a plurality of through-and-through channels is capped with a substantially flat green body at each of its faces to seal all the channels.
  • the openings of certain channels are then exposed through the cap at one face of the honeycomb and the remaining channels are exposed at the other face.
  • the composite capped structure is fired to sinter the base honeycomb and its end caps into a substantially integral body.
  • green refers to the state of the constituent ceramic materials, generally admixed together with binders and molded, prior to being fired or sintered.
  • the starting green ceramic honeycomb can be composed of any of the porous metal oxide materials that are well known to those skilled in the art for their moldability and sinterability into a structure having good mechanical strength and thermal properties.
  • porous metal oxide materials that are well known to those skilled in the art for their moldability and sinterability into a structure having good mechanical strength and thermal properties.
  • examples are zirconia, alumina, titania, cordierite, mullite, clay (preferably kaolin clay), talc, spinels, silicates such as lithium alumino-silicates, aluminates, aluminum titanate, aluminum titanate solid solutions, silica, glasses, and glass ceramics. Any mixture or combination of these materials can also be used.
  • the most preferred material for preparation into the starting green honeycomb of this invention is zirconia, preferably mixed with an oxide of calcium, magnesium, or yttrium in an amount that will wholly or partially stabilize the zirconia upon firing.
  • Zirconia is "wholly” or “partially” stabilized depending upon whether the amount of this stabilizing oxide is sufficient to form a cubic phase solid solution with all or only part of the zirconia.
  • calcia as little as 4 weight percent, based on the total calcia and zirconia weight, is sufficient to partially stabilize the zirconia, and about 10 weight percent is generally sufficient to fully stabilize it.
  • magnesia and yttria the corresponding ranges are about 3-21% by weight and about 4-16% by weight respectfully.
  • a material that is most easily processed according to the present invention is zirconia admixed with at least about 10 weight percent yttria and most preferably an amount of yttria sufficient to fully stabilize the zirconia.
  • the starting zirconia material has a residual silica content of not more than about 0.3 weight percent.
  • the constituent ceramic materials are admixed into a substantially homogeneous batch with about 1-30% by weight, based on the total batch weight, of a temporary binder.
  • the constituent ceramic materials are generally in particulate form, preferably of a size finer than 75 microns, and more preferably in a size finer than about 50 microns.
  • Any binder material conventionally used in ceramic catalyst support manufacture is suitable.
  • Preferred are binders that are decomposed and burned-off at temperatures of about 250-600°C. Examples are disclosed in: "Ceramic Processing Before Firing," ed/ by George Y. Onoda, Jr. & L.L.
  • a most preferred binder is methyl cellulose, one example of which is METHOCEL A4M, available from the Dow Chemical Co.
  • Mixing of the batch ingredients is preferably performed in a step-wise procedure in which any initially dry ingredients are first blended together.
  • This preliminary dry-blending operation can be performed in any conventional mixing equipment but the use of an intensive mixer having both barrel and mixing blade rotation is preferred.
  • the dry mixture is then plasticized by being further mixed, preferably in a mix muller, with a liquid medium (preferably water) which acts as a plasticizer.
  • a liquid medium preferably water
  • any remaining constituents are added.
  • Up to about 1% by weight, based upon total mixture weight, of a surfactant such as sodium stearate can also be added to facilitate mixing and flow for subsequent processing. Mixing of all constituents should be continued until a homogeneous or substantially homogeneous plasticized mass is obtained.
  • the plasticized batch is ultimately formed into the desired "green” honeycomb shape, preferably by extrusion through a die or by injection molding.
  • the monolithic honeycomb so-formed generally has two substantially flat surfaces or “faces” (together comprising, as hereinafter referred to, an "inlet face” and an “outlet face”) and a plurality of substantially parallel open channels that extend longitudinally through the honeycomb between the faces.
  • the transverse cross-sectional configuration of the channels is generally of any rounded (i.e. circular or elliptical) or polygonal (i.e., triangular; rectangular, preferably square; or hexagonal) shape.
  • the honeycomb contains 50-1000, more preferably about 100-400, of these through-and-through channels per square inch of inlet face surface area.
  • the transverse cross-sectional configuration of the honeycomb itself is preferably circular, elliptical, or hexagonal. Depending on its ultimately intended use, as those skilled in the art will recognize, the honeycomb can be shallower or deeper than it
  • the batch includes, as the ceramic materials, zirconia and sufficient magnesia, calcia, or yttria to provide the desired level of stabilization as described above.
  • the magnesia, calcia, or yttria component can be added in the form of a precursor compound, usually a salt, that is heat-decomposable to the metal oxide itself.
  • a precursor compound usually a salt
  • such precursor compounds are the metal oxylates, nitrates, carbonates, and acetates, and in the case of yttrium, the chloride salt as well.
  • the amount of precursor used is that which, after ultimate firing of the honeycomb structure, will generate an amount of corresponding stabilizing metal oxide, relative to the zirconia, that is sufficient to wholly or partially stabilize the zirconia as described above.
  • the zirconia and stabilizing metal oxide materials are preferably added to the batch in a particulate form finer than 10 microns, and preferably less than 1 micron.
  • a sintering aid can optionally be added to the batch in an amount of about 0.5-3.0 weight percent.
  • Preferred sintering aids are those that, upon firing and formation of the cubic zirconia, tend to form crystalline mullite or magnesium-aluminate spinel at the cubic grain boundaries.
  • the batch also contains about 3 weight percent of a temporary organic binder.
  • the extruded or injection-molded green honeycomb shape is generally dried at about 100-120°C, preferably by steam heat, to impart some rigidity and structural strength to the honeycomb for further processing according to the invention.
  • the green honeycomb thus formed is next fitted at each face with an end cap, formed of a body of a green ceramic material, in order to seal the channel openings.
  • the end caps are each prepared from a batch of plasticized ceramic material that is formed, for example by means of a press die or extrusion die, into a substantially flat body of a size and shape sufficient to completely cover the faces of the honeycomb. It is preferred that the end cap be about as thick as the partition walls that define the honeycomb channels and separate them from each other. This dimension is most preferably about 5-75 mils (about 0.013-0.19 cm).
  • the ceramic mixture used to form the end caps is preferably, but need not be, the same material from which the honeycomb itself is made and is most preferably taken from the same batch.
  • the shaped end caps will preferably not be dried prior to their application to the faces of the honeycomb but rather will be allowed to retain a plasticized consistency. In this state, the moisture content of the material is generally about 10-13% by weight.
  • each face of the dried green honeycomb is wetted, preferably with water, to re-plasticize the ceramic material at the face, and a still-wet end cap body is then firmly fitted onto each face with sufficient force to integrate the plasticized ceramic material of each into a substantially continuous phase. Any excess material from the end cap that extends beyond the sides of the honeycomb itself as a result of this pressing operation can be trimmed off so that the edges of the end caps are flush with the sides of the honeycomb.
  • the end caps are then selectively perforated to expose the openings of certain channels of the underlying honeycomb at the inlet face and the openings of the remainder of the channels at the outlet face of the honeycomb.
  • This can be effected by manual perforation of the end caps by a hand-held punch or tool having a pin that is sized and shaped appropriately to pierce the end cap in a manner congruent with the size and shape of the channel openings to be exposed.
  • this operation will be carried out automatically by, for example, imaging analysis in which an array of piercing pins, controlled by a processor connected to optical or other scanning means, is used to pierce the end caps to expose the desired openings.
  • the scanning means can optionally be equipped with a "penetrating" component such as an ultrasound or x-ray device, for location of the channels after the end cap has been applied.
  • a "penetrating” component such as an ultrasound or x-ray device
  • the faces of the honeycomb will be scanned, and signals corresponding to the location of the channels processed and stored, prior to fitting of the end caps.
  • Such automatic operation using an array of process tools or pins is particularly well suited for use when the selectively exposed channels at each face are to be regularly spaced such as in a "checkerboard" pattern or in a pattern of alternating rows of channels.
  • a suitable method and apparatus for control and piercing by image analysis is disclosed in U.S. Patent 4,557,773 (issued December 10, 1985, to Bonzo), which is hereby incorporated by reference.
  • the composite structure is then fired to harden and densify the material and to integrally join the end caps to the material of the honeycomb body itself.
  • the firing is performed at a temperature and for a time sufficient to effect actual sintering of the ceramic material.
  • the exact firing schedule as those skilled in the art will recognize, will be dictated primarily by the identity of the ceramic materials.
  • a preferred firing schedule is to heat the material to a temperature of about 1400°C over a 35-hour period; further heat from that temperature to a sintering temperature of about 1650-1800°C, preferably about 1750°C, over a 16-hour period; hold the material at the sintering temperature for about 4 hours; cool the material to about 1000°C over a 20-hour period; and then further cool the material from that temperature back to room temperature over about a 10-hour period.
  • FIG. 1 An example of a honeycomb thus formed with selectively sealed channels is shown in Figures 1 and 2.
  • the honeycomb designated generally as 1
  • the honeycomb has two end caps 2 adhering to and, upon firing and sintering, integrally forming a part of inlet face 3 and outlet face 4 of the honeycomb.
  • the end caps 2 are shown in exaggerated outline to indicate their disc-like shape. It will be understood, however, that after firing or sintering, the end caps will be integrally sealed to the honeycomb itself and there will generally be no discernible boundary between them, particularly when the end caps are of the same ceramic composition as the honeycomb.
  • the honeycomb has a plurality of channels 7, shown here in square cross-section, separated by thin partition walls, shown unnumbered.
  • honeycombs formed by the method of this invention are useful for any of the filtering or separation operations heretofore performed by honeycomb structures that have been designed for passage of the work fluid, or some component thereof, through the channel partition walls rather than end-to-end through the open channels themselves.
  • a novel application of such honeycombs takes advantage of the high surface area and solid electrolyte properties of certain ceramic materials and is directed to use of honeycombs formed by this invention as oxygen concentrators or fuel cells.
  • the honeycombs having selectively sealed channels as described above are coated with an electrically conductive material in a manner to connect the interior walls of the channels that are open at the inlet face and form from them a first electrode, and connect the interior walls of the channels that are open at the outlet face and form from them a second electrode.
  • an oxygen concentrator made by the present method air is introduced into the channels open at the inlet face, a first voltage is applied to the interior walls of those channels, and a second voltage is applied to the interior walls of the channels open at the outlet face, thereby creating an electrical potential across the ceramic material separating adjacent inlet-open and outlet-open channels. This electrical potential forces oxygen ions from the air through the channel walls, and concentrated oxygen is released into the outlet-open channels and collected at the outlet face.
  • the ceramic material selected for the preparation of the honeycomb body and the end caps is one which, prior to sintering, has a surface area of at least about 1.5 m2/g and which functions as a solid electrolyte that is permeable to oxygen ions but not to other components of air.
  • Examples are stabillized zirconia, preferably yttria-stabilized zirconia as described above, ⁇ -alumina, and mullite.
  • the electrically conductive material is applied to the composite honeycomb by conventional methods in a manner which will provide the inlet face and the interior walls of the inlet-open channels with a continuous coating, thereby forming a first electrode surface, and which will provide the outlet face and the interior walls of the outlet-open channels with a separate continuous coating, thereby forming a second, separate electrode surface.
  • Necessary characteristics of the electrode material are permeability to oxygen and stability and durability under operating conditions, which will generally be in the range of about 600-950°C. Examples of such materials are silver, platinum, lanthanum-strontium-manganite complexes, silver/palladium mixtures, and mixtures of silver/palladium and the lanthanum complexes.
  • the electrode material is generally dispersed in a suitable liquid carrier to form a paste or ink and then applied in suitable fashion by, for example, brush coating or dip coating.
  • the materials can be applied in powder form, such as a particulate mixture of silver and palladium, and the honeycomb structure then heated to a temperature sufficient to sinter or to melt and alloy the powders.
  • the electrode material is applied after the composite honeycomb itself has been sintered, but application of the electrode material in powdered form can, in appropriate cases, take place just prior to sintering so that the sintering of the ceramic and the sintering or melting/alloying of the electrical coating can take place in a single operation.
EP90119094A 1989-12-21 1990-10-05 Préparation de structures en nid d'abeille à obturation sélective de canaux Withdrawn EP0433582A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/454,524 US5062911A (en) 1989-12-21 1989-12-21 Preparation of ceramic honeycomb structure having selectively sealed channels
US454524 1989-12-21

Publications (1)

Publication Number Publication Date
EP0433582A1 true EP0433582A1 (fr) 1991-06-26

Family

ID=23804957

Family Applications (1)

Application Number Title Priority Date Filing Date
EP90119094A Withdrawn EP0433582A1 (fr) 1989-12-21 1990-10-05 Préparation de structures en nid d'abeille à obturation sélective de canaux

Country Status (4)

Country Link
US (1) US5062911A (fr)
EP (1) EP0433582A1 (fr)
JP (1) JPH04104807A (fr)
BR (1) BR9004744A (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7682578B2 (en) 2005-11-07 2010-03-23 Geo2 Technologies, Inc. Device for catalytically reducing exhaust
US7682577B2 (en) 2005-11-07 2010-03-23 Geo2 Technologies, Inc. Catalytic exhaust device for simplified installation or replacement
US7722828B2 (en) 2005-12-30 2010-05-25 Geo2 Technologies, Inc. Catalytic fibrous exhaust system and method for catalyzing an exhaust gas
EP2216084A1 (fr) * 2007-11-28 2010-08-11 NGK Insulators, Ltd. Procédé de liaison de structure d'étanchéité en nid d'abeille pour joints
US20190186851A1 (en) * 2010-09-22 2019-06-20 Raytheon Company Heat exchanger with a glass body

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2898364B2 (ja) * 1990-07-06 1999-05-31 日本碍子株式会社 電極一体型ハニカムヒーター及びその製造方法
US5266278A (en) * 1990-07-06 1993-11-30 Ngk Insulators, Ltd. Honeycomb heater having integrally formed electrodes and/or integrally sintered electrodes and method of manufacturing such honeycomb heater
US5487865A (en) * 1993-04-08 1996-01-30 Corning Incorporated Method of making complex shaped metal bodies
CN1093783C (zh) * 1996-02-21 2002-11-06 松下电器产业株式会社 液体喷涂喷嘴和液体喷涂喷嘴的制造方法
DE69939061D1 (de) 1998-06-12 2008-08-21 Aep Invest Inc Keramikbrennstoffzelle
EP1177092A4 (fr) * 1999-02-18 2004-11-17 Corning Inc Structure de verre de silice en nid d'abeilles fabriquee par extrusion de suies de silice
US6290757B1 (en) 1999-03-26 2001-09-18 Ceramphysics, Inc. Nitrogen purification device
US6354903B1 (en) * 1999-06-29 2002-03-12 Delphi Technologies, Inc. Method of manufacture of a plasma reactor with curved shape for treating auto emissions
US6878030B1 (en) * 1999-06-29 2005-04-12 Delphi Technologies, Inc. Plasma reactor for treating auto emissions—durable and low cost—curved shapes
US6824661B2 (en) 1999-09-23 2004-11-30 Ceramphysics, Inc. Combined oxygen and NOx sensor
US6592731B1 (en) 1999-09-23 2003-07-15 Ceramphysics, Inc. Amperometric oxygen sensor
JP4742405B2 (ja) * 2000-06-28 2011-08-10 トヨタ自動車株式会社 燃料改質装置
AU2002303452A1 (en) * 2001-04-23 2002-11-05 Dow Global Technologies Inc. Method of making wall-flow monolith filter
US6803015B2 (en) * 2001-04-23 2004-10-12 Dow Global Technologies Inc. Method of making wall-flow monolith filter
JP4097971B2 (ja) * 2002-03-28 2008-06-11 日本碍子株式会社 セラミックハニカム構造体の製造方法及びセラミックハニカム構造体
US7550221B2 (en) * 2003-10-29 2009-06-23 Rolls-Royce Fuel Cell Systems Limited Gas delivery substrate
KR100716369B1 (ko) * 2005-11-10 2007-05-11 현대자동차주식회사 디젤매연촉매여과필터의 제조방법
US7824602B2 (en) * 2006-03-31 2010-11-02 Massachusetts Institute Of Technology Ceramic processing and shaped ceramic bodies
US7614304B2 (en) * 2006-05-16 2009-11-10 Corning Incorporated Ultrasonic testing system and method for ceramic honeycomb structures
US8499633B2 (en) * 2006-05-16 2013-08-06 Corning Incorporated Non-contact ultrasonic testing method and device for ceramic honeycomb structures
US20070266547A1 (en) * 2006-05-16 2007-11-22 Zhiqiang Shi Pulse echo ultrasonic testing method for ceramic honeycomb structures
WO2011118669A1 (fr) * 2010-03-24 2011-09-29 日本碍子株式会社 Procédé de détection de matières particulaires
KR20150064745A (ko) * 2012-10-05 2015-06-11 이머리 세라믹 구조물
US20210032148A1 (en) * 2017-12-01 2021-02-04 Corning Incorporated Apparatus and method for producing glass

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0036321A1 (fr) * 1980-03-15 1981-09-23 Ngk Insulators, Ltd. Filtre céramique
EP0042301A1 (fr) * 1980-06-16 1981-12-23 Ngk Insulators, Ltd. Filtres céramiques ayant une structure en forme de nids d'abeilles et procédé pour leur fabrication
US4432918A (en) * 1981-08-24 1984-02-21 Corning Glass Works Methods for fabricating selectively plugged honeycomb structures
US4557773A (en) * 1981-07-15 1985-12-10 Corning Glass Works Method for selectively manifolding honeycomb structures

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4041591A (en) * 1976-02-24 1977-08-16 Corning Glass Works Method of fabricating a multiple flow path body
JPS577217A (en) * 1980-06-16 1982-01-14 Ngk Insulators Ltd Ceramic honeycomb filter and preparation thereof
US4329162A (en) * 1980-07-03 1982-05-11 Corning Glass Works Diesel particulate trap
US4846657A (en) * 1988-05-02 1989-07-11 Allied-Signal Inc. Die for extruding ultrafine honeycomb structures

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0036321A1 (fr) * 1980-03-15 1981-09-23 Ngk Insulators, Ltd. Filtre céramique
EP0042301A1 (fr) * 1980-06-16 1981-12-23 Ngk Insulators, Ltd. Filtres céramiques ayant une structure en forme de nids d'abeilles et procédé pour leur fabrication
US4557773A (en) * 1981-07-15 1985-12-10 Corning Glass Works Method for selectively manifolding honeycomb structures
US4432918A (en) * 1981-08-24 1984-02-21 Corning Glass Works Methods for fabricating selectively plugged honeycomb structures

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7682578B2 (en) 2005-11-07 2010-03-23 Geo2 Technologies, Inc. Device for catalytically reducing exhaust
US7682577B2 (en) 2005-11-07 2010-03-23 Geo2 Technologies, Inc. Catalytic exhaust device for simplified installation or replacement
US7722828B2 (en) 2005-12-30 2010-05-25 Geo2 Technologies, Inc. Catalytic fibrous exhaust system and method for catalyzing an exhaust gas
EP2216084A1 (fr) * 2007-11-28 2010-08-11 NGK Insulators, Ltd. Procédé de liaison de structure d'étanchéité en nid d'abeille pour joints
EP2216084A4 (fr) * 2007-11-28 2012-06-06 Ngk Insulators Ltd Procédé de liaison de structure d'étanchéité en nid d'abeille pour joints
US20190186851A1 (en) * 2010-09-22 2019-06-20 Raytheon Company Heat exchanger with a glass body

Also Published As

Publication number Publication date
BR9004744A (pt) 1991-09-10
US5062911A (en) 1991-11-05
JPH04104807A (ja) 1992-04-07

Similar Documents

Publication Publication Date Title
US5062911A (en) Preparation of ceramic honeycomb structure having selectively sealed channels
US5034023A (en) Ceramic honeycomb structures as oxygen separators or concentrators
CA2445107C (fr) Procede de fabrication d'un filtre monolithique a ecoulement sur la paroi
EP1385805B1 (fr) Procede de fabrication d'un filtre monolithique a ecoulement sur paroi
EP1769837B1 (fr) Structure en nid d'abeille ceramique et procede de fabrication de celle-ci
US6183609B1 (en) Sintered laminated structures, electrochemical cells and process for producing such sintered laminated structures
EP1745848A1 (fr) Corps à structure en nids d'abeille et dispositif de purification de gaz d'échappement
EP1703095A1 (fr) Dispositif d'epuration de gaz d'echappement et procede destine a regenerer un dispositif d'epuration de gaz d'echappement
EP2000194B1 (fr) Filtre en nids d'abeilles
EP0042302A1 (fr) Procédé pour la fabrication de filtres céramiques ayant une structure en forme de nids d'abeilles
JP3874443B2 (ja) パティキュレート捕集用フィルタ
US20080017034A1 (en) Process for producing a ceramic filter
EP2210867B1 (fr) Structure en nid d'abeilles et dispositif de purification utilisant la structure en nid d'abeilles
US20030160364A1 (en) Method for selectively plugging a honeycomb
JP3126939B2 (ja) 積層焼結体の製造方法
CN112569923A (zh) 复合氧化物催化剂、多孔质复合体以及复合氧化物催化剂的制造方法
EP4265315A1 (fr) Filtre à particules fines, procédé d'élimination de matériau particulaire des gaz d'échappement d'un moteur à combustion interne, et procédé de production d'un filtre à particules fines

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): BE DE FR IT SE

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 19911228